US5090324A - Warhead - Google Patents
Warhead Download PDFInfo
- Publication number
- US5090324A US5090324A US07/466,324 US46632490A US5090324A US 5090324 A US5090324 A US 5090324A US 46632490 A US46632490 A US 46632490A US 5090324 A US5090324 A US 5090324A
- Authority
- US
- United States
- Prior art keywords
- layer
- liner
- explosive
- shock wave
- warhead
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
Definitions
- the invention relates to a warhead provided with a shaped or projectile forming charge having a liner of a multiphase metallic material as a metal-metal laminate.
- the liner is produced in that ultra-fine particles of heavy metal, for example tungsten, are embedded in a carrier matrix of an ultrafine grain mixture (e.g. Al-Zn alloy).
- an ultrafine grain mixture e.g. Al-Zn alloy
- a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with the material being a tungsten-heavy metal alloy; and wherein the surface of the liner facing the explosive is disposed on a first plastic layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is lower than that of the liner.
- a second layer formed of a material having a high acoustic impedance, e.g. Armco iron, is disposed between the first layer and the explosive to couple the shock wave into the first layer.
- the invention is based on the idea of adapting the pressure profile of the shock wave to the material requirements of the liner by disposing a first layer in front of the liner on the side of the explosive.
- Particularly suitable are plastic layers. They exhibit favorable dispersion and absorption behavior for shock waves and therefore result in flattening of the otherwise very steep shock wave front. Additionally, they have a very low acoustic impedance.
- FIG. 1 is a schematic representation of a warhead including a prior art projectile forming liner.
- FIG. 2 shows the warhead of FIG. 1 with a first layer according to the invention.
- FIG. 3 shows the warhead of FIG. 2 with a second layer according to the invention.
- FIG. 4 is a schematic cross-sectional view of a warhead according to the invention with a shaped charge.
- the reference numeral 10 identifies the known warhead equipped with a projectile forming liner. It is essentially composed of a warhead casing 11, the explosive capsule with booster charge 12, the explosive 13 and the projectile forming liner 14.
- the liner 14 is composed, e.g., of copper and, after detonation of explosive 13, is reshaped into a contiguous projectile.
- a projectile formation is not possible if the liner is produced of a multi-phase metallic material or a metal-metal laminate.
- WHM tungsten heavy metal
- FIG. 2 shows a warhead 10' according to the invention which essentially differs from the warhead 10 of FIG. 1 only by the additional layer 15.
- the layer 15 not only causes flattening of the otherwise very steep shock wave front and damping of its amplitude, but also acoustic impedance matching to liner 14.
- layer 15 is composed of a plastic and particularly of a material having low acoustic impedance and good temperature resistance.
- Polyphenylene oxide (PPO) has been found to be particularly satisfactory in practice for this purpose.
- the thickness of layer 15 must be selected so that projectile forming liner 14, which would be destroyed in the conventional charge configuration, remains in effect due to the inventive measures.
- PPO having a thickness of 10 mm at the apex was employed as layer 15.
- the liner material was WHM.
- the shock wave will be reflected back and forth several times within the plastic layer so that the shock wave energy is successively coupled into the metal liner.
- a simple metal layer having a low acoustic impedance may also be employed (e.g., lead). This layer absorbs the components reflected at the phase interfaces of liner 14 and converts them to deformation work.
- a second, so-called coupling layer 16 may be employed in order to permit the incoming pressure wave to be transferred into layer 15 in the optimum manner.
- FIG. 3 Such an embodiment is shown in FIG. 3.
- the warhead is marked 10" and the coupling layer is marked 16.
- Such coupling layers 16 should preferably be composed of metals having a high acoustic impedance.
- the thickness of these layers is dependent on material and caliber and, in a practical embodiment, was, for example, 3 mm for a caliber of 35 mm. Armco iron was employed for the layer material.
- FIG. 4 shows the embodiment of a shaped charge equipped with intermediate layers according to the invention.
- the warhead is here marked 20, the warhead casing is marked 21, the explosive capsule with booster charge is marked 22 and the explosive is marked 23.
- the explosive is marked 23.
- first layer 25 in front of liner 24 on the side of the explosive, there is a first layer 25 as well as a coupling layer 26.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
- Radar Systems Or Details Thereof (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Vibration Dampers (AREA)
- Aerials With Secondary Devices (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
A warhead (10') which includes a shaped or projectile forming charge in the form of a liner (14) of a multi-phase metallic material or a metal-metal laminate. To prevent the liner (14) from being destroyed by the incoming shock wave and make impossible the formation of a projectile, that is, a shaped charge jet, a layer (15) is arranged, in front of the liner (14) on the side of the explosive, with the layer (15) causing the shock wave front to be flattened and damped and having an acoustic impedance which is lower than that of the liner (14).
Description
The invention relates to a warhead provided with a shaped or projectile forming charge having a liner of a multiphase metallic material as a metal-metal laminate.
Such warheads are disclosed, for example, in German Patent No. 2,927,556. The liner is produced in that ultra-fine particles of heavy metal, for example tungsten, are embedded in a carrier matrix of an ultrafine grain mixture (e.g. Al-Zn alloy).
When such multi-phase materials, particularly, however, those composed of tungsten-heavy metal alloys, such as, for example, W-Cu, WNiFeCo, are reshaped, the liners are frequently destroyed already at the onset of the profile or jet formation. The reason for this is, among others, that due to the great differences in acoustic impedance between the individual phases, the shock waves are reflected at the phase interfaces.
It is therefore an object of the present invention to further improve warheads of the above-mentioned type so that their liners are not destroyed by the incoming shock wave and therefore a projectile, that is, a shaped charge jet, is formed.
This object is accomplished according to the invention by a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with the material being a tungsten-heavy metal alloy; and wherein the surface of the liner facing the explosive is disposed on a first plastic layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is lower than that of the liner.
According to a further feature of the invention, a second layer formed of a material having a high acoustic impedance, e.g. Armco iron, is disposed between the first layer and the explosive to couple the shock wave into the first layer.
Further particularly advantageous features of the invention are disclosed in the dependent claims.
Thus, the invention is based on the idea of adapting the pressure profile of the shock wave to the material requirements of the liner by disposing a first layer in front of the liner on the side of the explosive. Particularly suitable are plastic layers. They exhibit favorable dispersion and absorption behavior for shock waves and therefore result in flattening of the otherwise very steep shock wave front. Additionally, they have a very low acoustic impedance.
Further details and advantages of the invention will be described below for embodiments thereof and with reference to the drawing figures.
FIG. 1 is a schematic representation of a warhead including a prior art projectile forming liner.
FIG. 2 shows the warhead of FIG. 1 with a first layer according to the invention.
FIG. 3 shows the warhead of FIG. 2 with a second layer according to the invention.
FIG. 4 is a schematic cross-sectional view of a warhead according to the invention with a shaped charge.
In FIG. 1, the reference numeral 10 identifies the known warhead equipped with a projectile forming liner. It is essentially composed of a warhead casing 11, the explosive capsule with booster charge 12, the explosive 13 and the projectile forming liner 14.
In conventional P charges, the liner 14 is composed, e.g., of copper and, after detonation of explosive 13, is reshaped into a contiguous projectile. As tests have shown, such a projectile formation is not possible if the liner is produced of a multi-phase metallic material or a metal-metal laminate. For example, it has not been possible in the past to produce a contiguous projectile of tungsten heavy metal (WHM) by employing WHM as the projectile forming liner 14.
FIG. 2 shows a warhead 10' according to the invention which essentially differs from the warhead 10 of FIG. 1 only by the additional layer 15.
As already described above, the layer 15 not only causes flattening of the otherwise very steep shock wave front and damping of its amplitude, but also acoustic impedance matching to liner 14.
Preferably, layer 15 is composed of a plastic and particularly of a material having low acoustic impedance and good temperature resistance. Polyphenylene oxide (PPO) has been found to be particularly satisfactory in practice for this purpose.
The thickness of layer 15 must be selected so that projectile forming liner 14, which would be destroyed in the conventional charge configuration, remains in effect due to the inventive measures. In a practical embodiment, PPO having a thickness of 10 mm at the apex was employed as layer 15. The liner material was WHM.
Since plastic layers generally have acoustic impedance values which are lower than those of metals and the explosive fumes, the shock wave will be reflected back and forth several times within the plastic layer so that the shock wave energy is successively coupled into the metal liner.
Instead of the plastic layer, a simple metal layer having a low acoustic impedance may also be employed (e.g., lead). This layer absorbs the components reflected at the phase interfaces of liner 14 and converts them to deformation work.
In addition to layer 15, a second, so-called coupling layer 16 may be employed in order to permit the incoming pressure wave to be transferred into layer 15 in the optimum manner. Such an embodiment is shown in FIG. 3. Here the warhead is marked 10" and the coupling layer is marked 16.
FIG. 4 shows the embodiment of a shaped charge equipped with intermediate layers according to the invention. The warhead is here marked 20, the warhead casing is marked 21, the explosive capsule with booster charge is marked 22 and the explosive is marked 23. In front of liner 24 on the side of the explosive, there is a first layer 25 as well as a coupling layer 26.
As in the above-described embodiments, it was possible with the aid of layer 25 to prevent liner 24 from being destroyed by the incoming shock wave which would have made the formation of a shaped charge jet impossible.
Claims (8)
1. In a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with said material being a tungsten-heavy metal alloy; the improvement wherein the surface of said liner facing said explosive is disposed on a first layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is substantially lower than that of said liner such that the shock wave will be reflected back and forth several times within said first layer, with said first layer being composed of polyphenylene oxide (PPO).
2. In a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with said material being a tungsten-heavy metal alloy; the improvement wherein the surface of said liner facing said explosive is disposed on a first layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is substantially lower than that of said liner such that the shock wave will be reflected back and forth several times within said first layer, with said first layer being composed of plastic, and further comprising a second layer having a high acoustic impedance disposed in front of the first layer on the side of the explosive for coupling the shock wave into said first layer.
3. A warhead according to claim 2, wherein said second layer is composed of a metallic material.
4. A warhead according to claim 3 wherein said second layer is formed of Armco iron.
5. In a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with said material being a tungsten-heavy metal alloy; the improvement wherein the surface of said liner facing said explosive is disposed on a first layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is lower than that of said liner, with said first layer being composed of plastic polyphenylene oxide (PPO).
6. In a warhead provided with a shaped or projectile forming charge arrangement including a casing containing an explosive and a liner of a multi-phase metallic material, with said material being a tungsten-heavy metal alloy; the improvement wherein the surface of said liner facing said explosive is disposed on a first layer which causes the shock wave front to be flattened and dampened and whose acoustic impedance is lower than that of said liner, with said first layer being composed of plastic; and further comprising a second layer having a high acoustic impedance disposed in front of the first layer on the side of the explosive for coupling the shock wave into said first layer.
7. A warhead according to claim 6, wherein said second layer is composed of a metallic material.
8. A warhead according to claim 7 wherein said second layer is formed of Armco iron.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3830347 | 1988-09-07 | ||
DE3830347A DE3830347C2 (en) | 1988-09-07 | 1988-09-07 | Warhead |
Publications (1)
Publication Number | Publication Date |
---|---|
US5090324A true US5090324A (en) | 1992-02-25 |
Family
ID=6362425
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US07/466,324 Expired - Fee Related US5090324A (en) | 1988-09-07 | 1989-06-08 | Warhead |
Country Status (7)
Country | Link |
---|---|
US (1) | US5090324A (en) |
EP (1) | EP0383858A1 (en) |
DE (1) | DE3830347C2 (en) |
ES (1) | ES2020022A6 (en) |
GR (1) | GR890100394A (en) |
PT (1) | PT91651A (en) |
WO (1) | WO1990002918A1 (en) |
Cited By (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5509356A (en) * | 1995-01-27 | 1996-04-23 | The Ensign-Bickford Company | Liner and improved shaped charge especially for use in a well pipe perforating gun |
US5567906A (en) * | 1995-05-15 | 1996-10-22 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5656791A (en) * | 1995-05-15 | 1997-08-12 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5705768A (en) * | 1992-12-24 | 1998-01-06 | Dyno Nobel Asia Pacific Limited | Shaped charges with plastic liner, concave recess and detonator means |
US5744747A (en) * | 1995-10-20 | 1998-04-28 | Giat Industries | Slug generating charge |
US5859383A (en) * | 1996-09-18 | 1999-01-12 | Davison; David K. | Electrically activated, metal-fueled explosive device |
US6021714A (en) * | 1998-02-02 | 2000-02-08 | Schlumberger Technology Corporation | Shaped charges having reduced slug creation |
US6186070B1 (en) * | 1998-11-27 | 2001-02-13 | The United States Of America As Represented By The Secretary Of The Army | Combined effects warheads |
US6349649B1 (en) | 1998-09-14 | 2002-02-26 | Schlumberger Technology Corp. | Perforating devices for use in wells |
US6460463B1 (en) | 2000-02-03 | 2002-10-08 | Schlumberger Technology Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance in a well |
US6668727B1 (en) * | 2003-06-18 | 2003-12-30 | The United States Of America As Represented By The Secretary Of The Navy | Explosively driven impactor grenade |
US20050011395A1 (en) * | 2003-05-27 | 2005-01-20 | Surface Treatment Technologies, Inc. | Reactive shaped charges and thermal spray methods of making same |
US7278354B1 (en) | 2003-05-27 | 2007-10-09 | Surface Treatment Technologies, Inc. | Shock initiation devices including reactive multilayer structures |
US20070295235A1 (en) * | 2006-06-27 | 2007-12-27 | Schlumberger Technology Corporation | Method and Apparatus for Perforating |
US20090078144A1 (en) * | 2007-09-21 | 2009-03-26 | Schlumberger Technology Corporation | Liner for shaped charges |
WO2009142789A2 (en) * | 2008-05-19 | 2009-11-26 | Raytheon Company | High-lethality low collateral damage forward firing fragmentation warhead |
WO2010056419A1 (en) * | 2008-11-17 | 2010-05-20 | Raytheon Company | Dual-mass forward and side firing fragmentation warhead |
US20110146523A1 (en) * | 2008-05-19 | 2011-06-23 | Raytheon Company | High-lethality low collateral damage fragmentation warhead |
US9243876B1 (en) * | 2014-07-22 | 2016-01-26 | Raytheon Company | Low-collateral damage directed fragmentation munition |
US9499895B2 (en) | 2003-06-16 | 2016-11-22 | Surface Treatment Technologies, Inc. | Reactive materials and thermal spray methods of making same |
CN106382864A (en) * | 2016-10-27 | 2017-02-08 | 北京航天长征飞行器研究所 | Shaped charge structure for active energy-containing composite shaped charge liner |
US10024642B2 (en) * | 2014-02-26 | 2018-07-17 | Saab Ab | Initiating device and method for manufacturing such a device |
US10683735B1 (en) * | 2019-05-01 | 2020-06-16 | The United States Of America As Represented By The Secretary Of The Navy | Particulate-filled adaptive capsule (PAC) charge |
US10844696B2 (en) | 2018-07-17 | 2020-11-24 | DynaEnergetics Europe GmbH | Positioning device for shaped charges in a perforating gun module |
US11021923B2 (en) | 2018-04-27 | 2021-06-01 | DynaEnergetics Europe GmbH | Detonation activated wireline release tool |
US11118880B2 (en) * | 2019-10-14 | 2021-09-14 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Fragmentation warhead for a missile |
US11480038B2 (en) | 2019-12-17 | 2022-10-25 | DynaEnergetics Europe GmbH | Modular perforating gun system |
US11753889B1 (en) | 2022-07-13 | 2023-09-12 | DynaEnergetics Europe GmbH | Gas driven wireline release tool |
US11808093B2 (en) | 2018-07-17 | 2023-11-07 | DynaEnergetics Europe GmbH | Oriented perforating system |
USD1010758S1 (en) | 2019-02-11 | 2024-01-09 | DynaEnergetics Europe GmbH | Gun body |
USD1019709S1 (en) | 2019-02-11 | 2024-03-26 | DynaEnergetics Europe GmbH | Charge holder |
US11946728B2 (en) | 2019-12-10 | 2024-04-02 | DynaEnergetics Europe GmbH | Initiator head with circuit board |
USD1034879S1 (en) | 2019-02-11 | 2024-07-09 | DynaEnergetics Europe GmbH | Gun body |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5565644A (en) * | 1995-07-27 | 1996-10-15 | Western Atlas International, Inc. | Shaped charge with wave shaping lens |
FR2793314B1 (en) * | 1996-04-02 | 2002-05-31 | Giat Ind Sa | CORE GENERATOR LOAD WITH IMPROVED PERFORMANCE |
DE102018006741B4 (en) | 2018-08-24 | 2022-06-15 | TDW Gesellschaft für verteidigungstecchnische Wirksysteme mbH | Tandem charge for a missile |
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US3224368A (en) * | 1964-09-10 | 1965-12-21 | Honeywell Inc | Dual liner shaped charge |
US3621916A (en) * | 1969-10-08 | 1971-11-23 | Shell Oil Co | Spark-type casing perforator |
US3760729A (en) * | 1971-12-21 | 1973-09-25 | Us Army | Hermetically sealed plastic cartridge case/cap system |
DE2336750A1 (en) * | 1973-07-19 | 1975-04-10 | Hans Walter Loeckmann | Hollow-charge armour-piercer - has pyrometal lining of cavity covered by layer of copper cadmium or plastics on both sides |
EP0105495A1 (en) * | 1982-09-30 | 1984-04-18 | Southwest Energy Group, Ltd., | Energy transfer through a multilayer liner for shaped charges |
US4747350A (en) * | 1984-06-18 | 1988-05-31 | Alexander Szecket | Hollow charge |
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DE2927555C1 (en) * | 1979-07-07 | 1985-05-09 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Molded charge lining and process for its manufacture |
DE2927556C1 (en) * | 1979-07-07 | 1985-05-09 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Shaped charge lining |
DE3528339A1 (en) * | 1985-08-07 | 1987-02-19 | Messerschmitt Boelkow Blohm | DEVICE FOR INITIATING A BLAST CHARGE |
-
1988
- 1988-09-07 DE DE3830347A patent/DE3830347C2/en not_active Expired - Fee Related
-
1989
- 1989-06-08 WO PCT/EP1989/000645 patent/WO1990002918A1/en not_active Application Discontinuation
- 1989-06-08 US US07/466,324 patent/US5090324A/en not_active Expired - Fee Related
- 1989-06-08 EP EP89907116A patent/EP0383858A1/en not_active Ceased
- 1989-06-13 GR GR890100394A patent/GR890100394A/en unknown
- 1989-07-11 ES ES8902441A patent/ES2020022A6/en not_active Expired - Lifetime
- 1989-09-07 PT PT91651A patent/PT91651A/en not_active Application Discontinuation
Patent Citations (8)
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US3162121A (en) * | 1960-10-31 | 1964-12-22 | Western Co Of North America | Explosive charge assemblies |
US3224368A (en) * | 1964-09-10 | 1965-12-21 | Honeywell Inc | Dual liner shaped charge |
US3621916A (en) * | 1969-10-08 | 1971-11-23 | Shell Oil Co | Spark-type casing perforator |
US3760729A (en) * | 1971-12-21 | 1973-09-25 | Us Army | Hermetically sealed plastic cartridge case/cap system |
DE2336750A1 (en) * | 1973-07-19 | 1975-04-10 | Hans Walter Loeckmann | Hollow-charge armour-piercer - has pyrometal lining of cavity covered by layer of copper cadmium or plastics on both sides |
EP0105495A1 (en) * | 1982-09-30 | 1984-04-18 | Southwest Energy Group, Ltd., | Energy transfer through a multilayer liner for shaped charges |
US4498367A (en) * | 1982-09-30 | 1985-02-12 | Southwest Energy Group, Ltd. | Energy transfer through a multi-layer liner for shaped charges |
US4747350A (en) * | 1984-06-18 | 1988-05-31 | Alexander Szecket | Hollow charge |
Cited By (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5705768A (en) * | 1992-12-24 | 1998-01-06 | Dyno Nobel Asia Pacific Limited | Shaped charges with plastic liner, concave recess and detonator means |
US5509356A (en) * | 1995-01-27 | 1996-04-23 | The Ensign-Bickford Company | Liner and improved shaped charge especially for use in a well pipe perforating gun |
WO1996022879A1 (en) * | 1995-01-27 | 1996-08-01 | The Ensign-Bickford Company | Improved liner and improved shaped charge especially for use in a well pipe perforating gun |
US5567906A (en) * | 1995-05-15 | 1996-10-22 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5656791A (en) * | 1995-05-15 | 1997-08-12 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5744747A (en) * | 1995-10-20 | 1998-04-28 | Giat Industries | Slug generating charge |
US5859383A (en) * | 1996-09-18 | 1999-01-12 | Davison; David K. | Electrically activated, metal-fueled explosive device |
US6021714A (en) * | 1998-02-02 | 2000-02-08 | Schlumberger Technology Corporation | Shaped charges having reduced slug creation |
US6349649B1 (en) | 1998-09-14 | 2002-02-26 | Schlumberger Technology Corp. | Perforating devices for use in wells |
US6186070B1 (en) * | 1998-11-27 | 2001-02-13 | The United States Of America As Represented By The Secretary Of The Army | Combined effects warheads |
US6460463B1 (en) | 2000-02-03 | 2002-10-08 | Schlumberger Technology Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance in a well |
US6523474B2 (en) | 2000-02-03 | 2003-02-25 | Schlumberger Technology Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance |
US20050011395A1 (en) * | 2003-05-27 | 2005-01-20 | Surface Treatment Technologies, Inc. | Reactive shaped charges and thermal spray methods of making same |
US7278354B1 (en) | 2003-05-27 | 2007-10-09 | Surface Treatment Technologies, Inc. | Shock initiation devices including reactive multilayer structures |
US7278353B2 (en) | 2003-05-27 | 2007-10-09 | Surface Treatment Technologies, Inc. | Reactive shaped charges and thermal spray methods of making same |
US20080173206A1 (en) * | 2003-05-27 | 2008-07-24 | Surface Treatment Technologies, Inc. | Reactive shaped charges comprising thermal sprayed reactive components |
US7658148B2 (en) | 2003-05-27 | 2010-02-09 | Surface Treatment Technologies, Inc. | Reactive shaped charges comprising thermal sprayed reactive components |
US9499895B2 (en) | 2003-06-16 | 2016-11-22 | Surface Treatment Technologies, Inc. | Reactive materials and thermal spray methods of making same |
US6668727B1 (en) * | 2003-06-18 | 2003-12-30 | The United States Of America As Represented By The Secretary Of The Navy | Explosively driven impactor grenade |
US20070295235A1 (en) * | 2006-06-27 | 2007-12-27 | Schlumberger Technology Corporation | Method and Apparatus for Perforating |
US8726809B2 (en) * | 2006-06-27 | 2014-05-20 | Schlumberger Technology Corporation | Method and apparatus for perforating |
US20090078144A1 (en) * | 2007-09-21 | 2009-03-26 | Schlumberger Technology Corporation | Liner for shaped charges |
US8156871B2 (en) * | 2007-09-21 | 2012-04-17 | Schlumberger Technology Corporation | Liner for shaped charges |
US7971535B1 (en) | 2008-05-19 | 2011-07-05 | Raytheon Company | High-lethality low collateral damage fragmentation warhead |
WO2009142789A2 (en) * | 2008-05-19 | 2009-11-26 | Raytheon Company | High-lethality low collateral damage forward firing fragmentation warhead |
US20110146523A1 (en) * | 2008-05-19 | 2011-06-23 | Raytheon Company | High-lethality low collateral damage fragmentation warhead |
US7930978B1 (en) | 2008-05-19 | 2011-04-26 | Raytheon Company | Forward firing fragmentation warhead |
JP2011521199A (en) * | 2008-05-19 | 2011-07-21 | レイセオン カンパニー | A forward-fired crushing warhead with high lethality and low incidental damage |
US20110094408A1 (en) * | 2008-05-19 | 2011-04-28 | Raythenn Company | Forward firing fragmentation warhead |
WO2009142789A3 (en) * | 2008-05-19 | 2010-01-14 | Raytheon Company | High-lethality low collateral damage forward firing fragmentation warhead |
WO2010056419A1 (en) * | 2008-11-17 | 2010-05-20 | Raytheon Company | Dual-mass forward and side firing fragmentation warhead |
US8006623B2 (en) | 2008-11-17 | 2011-08-30 | Raytheon Company | Dual-mass forward and side firing fragmentation warhead |
US20110179966A1 (en) * | 2008-11-17 | 2011-07-28 | Raytheon Company | Dual-mass forward and side firing fragmentation warhead |
US10024642B2 (en) * | 2014-02-26 | 2018-07-17 | Saab Ab | Initiating device and method for manufacturing such a device |
US9243876B1 (en) * | 2014-07-22 | 2016-01-26 | Raytheon Company | Low-collateral damage directed fragmentation munition |
CN106382864A (en) * | 2016-10-27 | 2017-02-08 | 北京航天长征飞行器研究所 | Shaped charge structure for active energy-containing composite shaped charge liner |
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Also Published As
Publication number | Publication date |
---|---|
GR890100394A (en) | 1990-10-31 |
PT91651A (en) | 1990-03-30 |
DE3830347C2 (en) | 1998-07-09 |
EP0383858A1 (en) | 1990-08-29 |
ES2020022A6 (en) | 1991-07-16 |
WO1990002918A1 (en) | 1990-03-22 |
DE3830347A1 (en) | 1990-03-08 |
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